EGNOS Space Segment

EGNOS
Title	EGNOS Space Segment
Edited by	GMV
Level	Basic
Year of Publication	2011

The EGNOS space segment is composed of four geostationary satellites (GEO) broadcasting corrections and integrity information for GPS satellites in the L1 frequency band (1575,42 MHz). At the date of publication the 4 GEOs used by EGNOS are:

• Inmarsat 3F2 AOR-E | PRN Number 120 | Orbital Slot 15.5 W
• Astra Ses-5 | PRN Number 136 | Orbital Slot 5 E
• Inmarsat 4F2 Emea | PRN Number 126 | Orbital Slot 64 E
• Astra-5B | PRN Number 123 | Orbital Slot 31.5 E

EGNOS GEO satellites SES-5 (PRN 136) and INMARSAT 3F2 AOR-E (PRN 120) are currently part of the EGNOS operational platform and are transmitting the operational Signal-In-Space (SIS) to be used by EGNOS users. ASTRA-5B (PRN 123) and INMARSAT 4F2 EMEA (PRN 126) are part of the EGNOS TEST Platform broadcasting the TEST SIS. This space segment configuration provides a high level of redundancy over the whole service area in case of a geostationary satellite link failure. The EGNOS operations are handled in such a way that, at any point in time, at least two of the four GEOs broadcast an operational signal. Since it is only necessary to track a single GEO satellite link to benefit from the EGNOS Services, this secures a switching capability in case of interruption and ensures a high level of continuity of service.

Coverage of EGNOS of GEOs with 5 degrees masking angle

It is intended that the EGNOS space segment will be replenished over time in order to maintain a similar level of redundancy. The exact orbital location of future satellites may vary, though this will not impact the service offered to users. Similarly, different PRN code numbers may be assigned to future GEOs. It is important to remark that these changes in the EGNOS GEO space segment are performed in a seamless manner without any interruption from an EGNOS user point of view and without compromising at any moment the EGNOS performances. The services will be made available from the provision of new signals from the last EGNOS transponders generation embarked on-board the SES-5 and ASTRA-5B geostationary satellites. Both satellites are capable of transmitting dual-frequency signals compliant with GPS L1/L5 and Galileo E1/E5 signal specifications, but these new signals will be introduced into the EGNOS service provision only for L1 between 2015 and 2016.

The main criteria followed in the selection of the satellites positions have been:

• Improve the measurement geometry and hence the system availability.
• Maximise the visibility angle diversity and hence minimise the risk of signal blocking.
• Provide dual geostationary coverage (minimum) within the core service area.

The Inmarsat-3 Satellite-Navigation Mission

Inmarsat-3 Navigation Payload block diagram

Inmarsat’s Third Generation satellites carry a navigation payload which is used by EGNOS.

The first Inmarsat-3 (F2 AOR-E) satellite carrying an EGNOS transponder was launched in September 1996 (PRN 120) while the second one, Inmarsat-3 F5 IOR-W, was launched in February 1998 (PRN 126).

Inmarsat-3s were built by Lockheed Martin Astro Space (now Lockheed Martin Missiles & Space) of the USA, responsible for the basic spacecraft, and the European Matra Marconi Space (now Astrium), which developed the communications payload, being the first satellite launched by the Proton launch vehicle. From 30 August 2018 the Inmarsat-3 satellite is switched off and in Test mode status.

The Inmarsat-4 Satellite-Navigation Mission

Inmarsat’s Forth Generation satellites carry a navigation payload which is used by EGNOS. The first Inmarsat-4 (IOR) were built by Lockheed Martin and was launched in 11 March 2005 at orbital position 143, 5º East, using the Atlas V rocket. This satellite was launched with the intention of providing BGAN and GSPS services and also for bands wide rent. After that, a second satellite (AOR-West) was launched in 8 November 2005 at orbital position 53º West, in order to complement the BGAN and GSPS services aforementioned. The launch was made with a Proton-M/Briz-M rocket. Finally, the Third phase of Inmarsat-4 was launched in 18 August 2008 at orbital position 98º West, by a Proton rocket.

Astra Ses-5

Astra SES-5 is a commercial geostationary communication satellite operated by SES. It was launched on 9 July 2012 at orbital position 5º East. The launch was made with a Proton-M/Briz-M rocket from the Baikonur air base in Kazajistan. It was constructed by Space Systems/Loral, and is based on the LS-1300 satellite bus. The satellite is equipped with 24-C band (36MHz) and 36 Ku-band (33-36MHz) transponders. This satellite was born with the intention of improving the capacity for DTH (Direct to Home) and EGNOS services. The mission programmed duration is 15 years and the coverage area comprises of Sub-Saharan Africa, North Africa, Europe and Middle East Atlantic Ocean.

Astra-5B

Astra-5B coverage

The Astra-5B satellite officially came into service in June 2014 at orbital position 31.5º East. The Astra 5B was launched into space on 22 March 2014. The launch was made with an Ariane 5 rocket from the Kourou air base in French Guiana. The satellite is equipped with 40 Ku-band transponders (equivalent to 36MHz) and 6 Ka-band transponders. In addition this new transponder will support the next EGNOS generation (EGNOS V3) that will provide dual-frequency signals on both bands L1 and L5 and augment both GPS and Galileo. This satellite was born with the intention of improving the capacity for DTH (Direct to Home) services. Also for the capacity of cable services. They also feed digital terrestrial television networks in Central Europe, Eastern Europe and in particular Russia and neighbouring markets. The Astra-5B was the 56th satellite in the SES fleet. It has two coverage beams, Wide and High Power. The High Power can be captured in the westernmost part of Europe, as can be seen in the image.